{"title":"基于Simulink/Aerosim的无人机动态仿真模型建立方法","authors":"Guoshao Chen, Zhongsheng Wang, Sen Yang","doi":"10.1109/ICCNEA.2017.17","DOIUrl":null,"url":null,"abstract":"Aiming at the problem of UAV dynamic modeling with high difficulty and poor timeliness, a UAV dynamic model based on Simulink/Aerosim rapid method is established in this paper. Based on the analysis of UAV system internal structure, using Simulink/Aerosim toolbox to build six degrees of freedom dynamic simulation model of unmanned aerial vehicle and the setting of relevant parameters and RTW environment configuration process is analyzed, finally, by analyzing the typical flight parameters of a certain type UAV in ideal environment and wind interference environment, the feasibility and validity of the method is illustrated.","PeriodicalId":113898,"journal":{"name":"2017 International Conference on Computer Network, Electronic and Automation (ICCNEA)","volume":"171 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2017-09-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"UAV Dynamic Simulation Model Stablishment Method Based on Simulink/Aerosim\",\"authors\":\"Guoshao Chen, Zhongsheng Wang, Sen Yang\",\"doi\":\"10.1109/ICCNEA.2017.17\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"Aiming at the problem of UAV dynamic modeling with high difficulty and poor timeliness, a UAV dynamic model based on Simulink/Aerosim rapid method is established in this paper. Based on the analysis of UAV system internal structure, using Simulink/Aerosim toolbox to build six degrees of freedom dynamic simulation model of unmanned aerial vehicle and the setting of relevant parameters and RTW environment configuration process is analyzed, finally, by analyzing the typical flight parameters of a certain type UAV in ideal environment and wind interference environment, the feasibility and validity of the method is illustrated.\",\"PeriodicalId\":113898,\"journal\":{\"name\":\"2017 International Conference on Computer Network, Electronic and Automation (ICCNEA)\",\"volume\":\"171 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2017-09-01\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"2017 International Conference on Computer Network, Electronic and Automation (ICCNEA)\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/ICCNEA.2017.17\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"2017 International Conference on Computer Network, Electronic and Automation (ICCNEA)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/ICCNEA.2017.17","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
UAV Dynamic Simulation Model Stablishment Method Based on Simulink/Aerosim
Aiming at the problem of UAV dynamic modeling with high difficulty and poor timeliness, a UAV dynamic model based on Simulink/Aerosim rapid method is established in this paper. Based on the analysis of UAV system internal structure, using Simulink/Aerosim toolbox to build six degrees of freedom dynamic simulation model of unmanned aerial vehicle and the setting of relevant parameters and RTW environment configuration process is analyzed, finally, by analyzing the typical flight parameters of a certain type UAV in ideal environment and wind interference environment, the feasibility and validity of the method is illustrated.